Orbit Fit and Astrometric record for 00QJ226

The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.

# Object: 00QJ226   
# Created Fri May  2 02:36:32 2008
# Orbit generated from Bernstein formalism
# Fitting    7 observations of    7
# Arc:   1.24d
# First observation: 2000/08/29
#  Last observation: 2000/08/30
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     4.25 DOF:   10 RMS:  0.14
# Min/Max residuals:    -0.26    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.651752E-05  2.720988E-02 -3.316981E-06 -4.523181E-03  2.705877E-02  0.000000E+00
# Covariance matrix:
  4.0688E-11  6.8057E-08 -5.6270E-14 -1.6227E-12  1.0971E-08  0.0000E+00
  6.8057E-08  1.1608E-04 -9.5878E-11 -2.5959E-09  1.8641E-05  0.0000E+00
 -5.6270E-14 -9.5878E-11  5.2375E-13 -1.8982E-10 -1.5401E-11  0.0000E+00
 -1.6227E-12 -2.5959E-09 -1.8982E-10  1.1482E-07 -4.2410E-10  0.0000E+00
  1.0971E-08  1.8641E-05 -1.5401E-11 -4.2410E-10  2.9966E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  2.6070E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.842693  -21.496758    0.048725   -0.014953   -1.005292  2451785.629173
# Heliocentric elements and errors
Epoch:              2451780.5000  =  2000/08/24
Mean Anomaly:          282.76242 +/-   311.558
Argument of Peri:      262.70186 +/-    22.441
Long of Asc Node:      153.51253 +/-     1.970
Inclination:             9.46629 +/-     3.715
Eccentricity:         0.00438746 +/-    0.5853
Semi-Major Axis:     38.00172739 +/-   19.7207
Time of Perihelion: 2470138.6790 +/- 1785324.1
Perihelion:          37.83499627 +/-   29.6676
Aphelion:            38.16845851 +/-   29.7824
Period (y)              234.2681 +/-    182.36
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           35.30554002 +/-    2.1995
Ecliptic Y          -13.95008175 +/-    0.8665
Ecliptic Z           -0.54366146 +/-    0.0348
Ecliptic XDOT         0.00099532 +/-    0.0016
Ecliptic YDOT         0.00256938 +/-    0.0010
Ecliptic ZDOT        -0.00045746 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   37.96553049 +/-    2.0700
Geocenter to KBO     36.95659211 +/-    2.3643
# Hcoef:  8.14

The following table shows the complete astrometric record for 00QJ226. The first three columns show the date of observation. The next six columns are RA and DEC. The next column (when provided) is the observed magnitude and filter. The next column is the object name (00QJ226) followed by the observatory code and reference code for the source of the astrometry.

2000 08  29.12843  22 41 48.53   -09 09 46.6         00QJ226   809  Cb8401      
2000 08  29.22378  22 41 48.08   -09 09 49.8         00QJ226   809  Cb8401      
2000 08  30.10532  22 41 43.72   -09 10 18.5         00QJ226   809  Cb8401      
2000 08  30.19597  22 41 43.27   -09 10 21.1   23.5R 00QJ226   809  Cb8401      
2000 08  30.27500  22 41 42.88   -09 10 23.6         00QJ226   809  Cb8401      
2000 08  30.32187  22 41 42.65   -09 10 25.1         00QJ226   809  Cb8401      
2000 08  30.36952  22 41 42.42   -09 10 26.7         00QJ226   809  Cb8401      

The following table shows the residuals to the orbit fit. The first coumn is the point number. The second column is the time, in years, measured from the first observation. The third and fifth columns are the regularized positions used in the orbit fit. The fourth and sixth columns are the residuals, in arc seconds, for RA and Dec respectively.

  1   0.0000      0.00    -0.13       0.00     0.14
  2   0.0003     -7.38     0.21      -0.47    -0.12
  3   0.0027    -77.99    -0.26      -2.87    -0.21
  4   0.0029    -85.15    -0.08      -2.79     0.08
  5   0.0031    -91.44     0.02      -2.94     0.09
  6   0.0033    -95.16     0.08      -3.05     0.07
  7   0.0034    -98.91     0.16      -3.26    -0.04

The following table comes from a 10My integration of the orbit of the object. Three columns are shown. The first column is the result of integrating the nominal orbit. The other two columns are based on clones of the nominal orbit that are +/- 3 sigma from the nominal orbit. If all three types agree then the classificiation is deemed secure. The basis for these calculations is described in more detail in AJ, 129, 1117 (2005). Any use made of these calculations should refer to and credit this publication and the Deep Ecliptic Survey Team.

00QJ226    quality flag:2

Type:       CENTAURR  CENTAURR   REMOVED

axisobj       39.980    39.980    39.980
ecceobj        0.194     0.194     0.194
incobj         9.389     9.389     9.389
qmin          29.148    29.336    30.242
qmax          57.086    58.555    48.396
amean         38.040    40.249    36.357
amin          31.730    36.474    32.379
amax          44.192    45.280    40.262
emean          0.159     0.223     0.107
emin           0.002     0.154     0.041
emax           0.293     0.315     0.204
imean          7.117     8.872     8.394
imin           4.145     5.761     6.378
imax           8.602    11.631     9.959
fracstop       0.675     0.680     0.619
cjmean         2.992     2.975     2.989

libcent 0     -180.0    -180.0    -180.0
libamp  0     -180.0    -180.0    -180.0
libcent 1     -180.0    -180.0    -180.0
libamp  1     -180.0    -180.0    -180.0
libcent 2     -180.0    -180.0    -180.0
libamp  2     -180.0    -180.0    -180.0
libcent 3     -180.0    -180.0    -180.0
libamp  3     -180.0    -180.0    -180.0
libcent 4     -180.0    -180.0    -180.0
libamp  4     -180.0    -180.0    -180.0

kozaimean      189.2     180.0     179.5
kozaiamp       180.0     180.0     180.0